GB592591A - Improvements in locking devices - Google Patents

Improvements in locking devices

Info

Publication number
GB592591A
GB592591A GB1713644A GB1713644A GB592591A GB 592591 A GB592591 A GB 592591A GB 1713644 A GB1713644 A GB 1713644A GB 1713644 A GB1713644 A GB 1713644A GB 592591 A GB592591 A GB 592591A
Authority
GB
United Kingdom
Prior art keywords
pin
keeper
slot
detent
members
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1713644A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JOHN HUNTER LOWDEN
MILES AIRCRAFT Ltd
Original Assignee
JOHN HUNTER LOWDEN
MILES AIRCRAFT Ltd
Filing date
Publication date
Application filed by JOHN HUNTER LOWDEN, MILES AIRCRAFT Ltd filed Critical JOHN HUNTER LOWDEN
Publication of GB592591A publication Critical patent/GB592591A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/20Operating mechanisms mechanical

Abstract

592,591. Hinges; catches. MILES AIRCRAFT, Ltd., and LOWDEN, J. H. Sept. 7, 1944, No. 17136. [Classes 44 and 65 (ii)] [Also in Group XXXIII] In a locking device for locking two members together, e.g. hinged members of an aircraft undercarriage, comprising a pin 4, Fig. 1, on the member 1, extending transversely to the general direction of relative movement between the members, and engaging in an open-ended slot 8 in a keeper 6 housed in the other member 2 and rotatable between a position in which the slot is open for the entry or exit of the pin and a locking position in which the slot retains the pin, with a releasable detent 11 normally holding the keeper 6 in the locking position, the keeper is of circular form with its periphery forming its bearing surface in the member 2. The slot 8 may have one edge so arranged that the keeper is rotated to locking position on engagement by the pin 4, and may also have a second edge so arranged that the pin rotates the keeper to the open position when the detent is released and the members are folded about the hinge-pin 3. The pin 4 and the hinge-pin 3 extend between cheeks on the end of the member 1, and the flattened end of the member 2, in which the keeper 6 and the detent 11 are housed, fits between these cheeks. An open-ended slot 5 in the member 2 permits entry of the pin 4. The detent may be operable by means of a bell-crank lever 15 which is actuated by a link 16 pivoted to a sleeve 13 sliding on the member 2 and moved by the operating member 27 which effects the folding of the members. A spring-pressed plunger 28 bears on the periphery of the keeper 6 to prevent free rotation to the closed position. In the construction shown in Fig. 6, the keeper 6 is biassed towards the open position by a spring 17, and the detent is a spring-urged plunger 21 having pin and slot connection with the sliding sleeve 13.
GB1713644A 1944-09-07 Improvements in locking devices Expired GB592591A (en)

Publications (1)

Publication Number Publication Date
GB592591A true GB592591A (en) 1947-09-23

Family

ID=1732858

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1713644A Expired GB592591A (en) 1944-09-07 Improvements in locking devices

Country Status (1)

Country Link
GB (1) GB592591A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015036730A1 (en) * 2013-09-10 2015-03-19 Messier-Dowty Limited Aircraft landing gear assembly with a ground lock
US10967959B2 (en) 2017-09-13 2021-04-06 General Atomics Aeronautical Systems, Inc. Folding trailing arm landing gear

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015036730A1 (en) * 2013-09-10 2015-03-19 Messier-Dowty Limited Aircraft landing gear assembly with a ground lock
EP3566944A1 (en) * 2013-09-10 2019-11-13 Safran Landing Systems UK Limited Aircraft landing gear assembly with a ground lock
EP3584158A1 (en) * 2013-09-10 2019-12-25 Safran Landing Systems UK Limited Aircraft landing gear assembly with a ground lock
US10569863B2 (en) 2013-09-10 2020-02-25 Safran Landing Systems Uk Ltd Lock and aircraft landing gear assembly
US11242137B2 (en) 2013-09-10 2022-02-08 Safran Landing Systems Uk Ltd Lock and aircraft landing gear assembly
US10967959B2 (en) 2017-09-13 2021-04-06 General Atomics Aeronautical Systems, Inc. Folding trailing arm landing gear
US11530031B2 (en) 2017-09-13 2022-12-20 General Atomics Aeronautical Systems, Inc. Folding trailing arm landing gear
US11932379B2 (en) 2017-09-13 2024-03-19 General Atomics Aeronautical Systems, Inc. Folding trailing arm landing gear

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